NASA NTRS · 19990019399
Unlined Reuseable Filament Wound Composite Cryogenic Tank Testing
Abstract
An unlined reusable filament wound composite cryogenic tank was tested at the Marshall Space Flight Center using LH2 cryogen and pressurization to 320 psig. The tank was fabricated by Phillips Laboratory and Wilson Composite Group, Inc., using an EnTec five-axis filament winder and sand mandrels. The material used was IM7/977-2 (graphite/epoxy).
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Murphy, A. W., Lake, R. E., Wilkerson, C.. 1999-01-01. Unlined Reuseable Filament Wound Composite Cryogenic Tank Testing. https://ntrs.nasa.gov/citations/19990019399
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